Erosive Burning of Aluminized Composite Propellants: X-Ray Absorption Measurement, Correlation, and Application
Author:
Affiliation:
1. NOF Corporation, Taketoyo, Aichi 470-2398, Japan
2. Tokai University, Hiratsuka, Kanagawa 259-1292, Japan
3. Japan Aerospace Exploration Agency, Sagamihara, Kanagawa 229-8510, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.7950
Reference19 articles.
1. Erosive burning of solid propellants
2. Ultrasonic measurements of solid propellant burning rates in nozzleless rocket motors
3. Ultrasound measurement method: Errors, noise, and sensitivity
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